Inherent Characteristic and Steady Response Analysis of Aviation Gear with Thin-spoke
The thin- spoke structure gear model is established by using 3D modeling software,and the finite element software is used for the pre- processing. The load history on single tooth is obtained according to the dynamics equation and load distribution,which is applied on the basis of meshing time. By t...
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| Format: | Article |
| Language: | zho |
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Editorial Office of Journal of Mechanical Transmission
2016-01-01
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| Series: | Jixie chuandong |
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| Online Access: | http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2016.05.033 |
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| author | Wang Dayong |
| author_facet | Wang Dayong |
| author_sort | Wang Dayong |
| collection | DOAJ |
| description | The thin- spoke structure gear model is established by using 3D modeling software,and the finite element software is used for the pre- processing. The load history on single tooth is obtained according to the dynamics equation and load distribution,which is applied on the basis of meshing time. By this means,the force condition of gear under operation condition is simulated. The inherent characteristic of gear with thin-spoke is calculated,the graph of travelling waves is plotted. The steady responses and dynamic stress under operation condition and resonance speed is calculated through the method of modal superposition and the curve of dynamic stress is drawn. This method applies to analyze steady responses under different speed conditions of any kinds of gear. It provides reference for stress check and optimum structure. |
| format | Article |
| id | doaj-art-df1d7137b41e4afa9e67ad598615a6e4 |
| institution | Kabale University |
| issn | 1004-2539 |
| language | zho |
| publishDate | 2016-01-01 |
| publisher | Editorial Office of Journal of Mechanical Transmission |
| record_format | Article |
| series | Jixie chuandong |
| spelling | doaj-art-df1d7137b41e4afa9e67ad598615a6e42025-01-10T14:17:39ZzhoEditorial Office of Journal of Mechanical TransmissionJixie chuandong1004-25392016-01-014014514729923818Inherent Characteristic and Steady Response Analysis of Aviation Gear with Thin-spokeWang DayongThe thin- spoke structure gear model is established by using 3D modeling software,and the finite element software is used for the pre- processing. The load history on single tooth is obtained according to the dynamics equation and load distribution,which is applied on the basis of meshing time. By this means,the force condition of gear under operation condition is simulated. The inherent characteristic of gear with thin-spoke is calculated,the graph of travelling waves is plotted. The steady responses and dynamic stress under operation condition and resonance speed is calculated through the method of modal superposition and the curve of dynamic stress is drawn. This method applies to analyze steady responses under different speed conditions of any kinds of gear. It provides reference for stress check and optimum structure.http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2016.05.033Aviation gearThin-spoke structureInherent characteristicSteady responseDynamic stress |
| spellingShingle | Wang Dayong Inherent Characteristic and Steady Response Analysis of Aviation Gear with Thin-spoke Jixie chuandong Aviation gear Thin-spoke structure Inherent characteristic Steady response Dynamic stress |
| title | Inherent Characteristic and Steady Response Analysis of Aviation Gear with Thin-spoke |
| title_full | Inherent Characteristic and Steady Response Analysis of Aviation Gear with Thin-spoke |
| title_fullStr | Inherent Characteristic and Steady Response Analysis of Aviation Gear with Thin-spoke |
| title_full_unstemmed | Inherent Characteristic and Steady Response Analysis of Aviation Gear with Thin-spoke |
| title_short | Inherent Characteristic and Steady Response Analysis of Aviation Gear with Thin-spoke |
| title_sort | inherent characteristic and steady response analysis of aviation gear with thin spoke |
| topic | Aviation gear Thin-spoke structure Inherent characteristic Steady response Dynamic stress |
| url | http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2016.05.033 |
| work_keys_str_mv | AT wangdayong inherentcharacteristicandsteadyresponseanalysisofaviationgearwiththinspoke |